Fuel nozzle having swirler-integrated radial fuel jet
a fuel nozzle and swirler technology, which is applied in the ignition of the turbine/propulsion engine, engine starters, lighting and heating apparatus, etc., can solve the problems of reducing the functionality of the fuel nozzle, affecting the operation of the turbine engine, and insufficient and problemati
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[0013]FIG. 1 illustrates an exemplary turbine engine 10. Turbine engine 10 may be associated with a stationary or mobile work machine configured to accomplish a predetermined task. For example, turbine engine 10 may embody the primary power source of a generator set that produces an electrical power output or of a pumping mechanism that performs a fluid pumping operation. Turbine engine 10 may alternatively embody the prime mover of an earth-moving machine, a passenger vehicle, a marine vessel, or any other mobile machine known in the art. Turbine engine 10 may include a compressor section 12, a combustor section 14, a turbine section 16, and an exhaust section 18.
[0014]Compressor section 12 may include components rotatable to compress inlet air. Specifically, compressor section 12 may include a series of rotatable compressor blades 22 fixedly connected about a central shaft 24. As central shaft 24 is rotated, compressor blades 22 may draw air into turbine engine 10 and pressurize t...
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